GB202118A - Improvements in or relating to the surfaces of aircraft members - Google Patents

Improvements in or relating to the surfaces of aircraft members

Info

Publication number
GB202118A
GB202118A GB1734822A GB1734822A GB202118A GB 202118 A GB202118 A GB 202118A GB 1734822 A GB1734822 A GB 1734822A GB 1734822 A GB1734822 A GB 1734822A GB 202118 A GB202118 A GB 202118A
Authority
GB
United Kingdom
Prior art keywords
covering
discs
ribs
fabric
pins
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB1734822A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB1734822A priority Critical patent/GB202118A/en
Publication of GB202118A publication Critical patent/GB202118A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/26Construction, shape, or attachment of separate skins, e.g. panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)

Abstract

202,118. Robinson, E. June 23, 1922. Planes, construction of.-The fabric or other covering 12 is secured to the ribs &c. of aircraft wings or other members by discs 4 having flat upper surface, and convex or bevelled under surfaces which are screwed on to the threaded end 5 of pins 6 to press the covering into correspondingly-shaped recesses 11 formed at intervals in the flanges 9 of the ribs &c. The discs 4, which are flush with the surface when screwed home, are locked by strips of fabric 14 doped over the main covering. The inner ends of the pins 6 have wood-screws 8, and a flange may be formed between the two screws to assist in holding the flange member 9 of the rib in position.
GB1734822A 1922-06-23 1922-06-23 Improvements in or relating to the surfaces of aircraft members Expired GB202118A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1734822A GB202118A (en) 1922-06-23 1922-06-23 Improvements in or relating to the surfaces of aircraft members

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1734822A GB202118A (en) 1922-06-23 1922-06-23 Improvements in or relating to the surfaces of aircraft members

Publications (1)

Publication Number Publication Date
GB202118A true GB202118A (en) 1923-08-16

Family

ID=10093596

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1734822A Expired GB202118A (en) 1922-06-23 1922-06-23 Improvements in or relating to the surfaces of aircraft members

Country Status (1)

Country Link
GB (1) GB202118A (en)

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